PRGB/TAGB Oil Temperature Limits (Single Engine)

General Rotor Speed (Nr) Limits

-Max airspeed for 100% Nr is 220 KCAS-Max altitude for 100% Nr is 17,000 ft DA-Nr shall be above 75% before starting 2nd Engine*SFD may indicate RPM HIGH condition when one does not actually exist. Refer to CDU and DEU for correct Nr.

CAUTION: During high power settings, possible proprotor overtorque may occur with excessive ________ ________ _______.

lateral cyclic inputs

CAUTION: Delay takeoff until gearbox oil temperatures reach ___

20° C

20° C

22

NOTE: For 100% or 104% Nr, PRTR OVERTORQUE (L/R) will post when either Qm is >___ for ___ seconds or >___ Qm instantaneous. For 84% Nr, PRTR OVERTORQUE (L/R) will post when either Qm is > ___ for ___ seconds or > ___ Qm instantaneous.

re-referenceinstantaneous

Flight is prohibited with hydraulic fluid temperature below ____.

-18° C

Hydraulic Pressure Limits

Generator Operation Range

-Generators 1* and 2 Trip on at 72% Nr and off at 67%** Nr.-Generators 3 and 4 Trip on at 82% Nr and off at 80-82% Nr.*If APU engaged, GEN 1 unaffected by Nr.**May remain on for values below 67% Nr, the trip value will be determined by load and frequency.

27

Regulated converters shall be started above ____. Once started above ___, regulated converters are limited to a continuous operational OAT of ____ to ____. The converters are limited to ___ minutes of operation from ___ to ___.

-40°C; -40°C; -54°C to 50°C30 minutes; 55°C to 71°C

28

For operations without domed searchlight cover, ensure searchlights are turned off and allowed to cool for ___ ______ prior to performing refueling operations (air or ground).

2 minutes

29

The search/landing lights shall not be operated in ______ ______ ______ without proprotors turning.

Unprepared grassy areas

30

The searchlights shall not be motorized to/from the extended position above ___ kts.

200 kts

31

Flight outside of the ______ ______ ______ is prohibited. Commanding maximum rate ______ ______ at the Vcon limits is prohibited.

Conversion protection limitsAft nacelle

32

WARNING: Flight outside of the ______ ______ ______ limits may result in in-flight structural damage.

Upper conversion protection

33

Flight with nacelles between ___ and ___ is limited to relative crosswinds less than ___ kts and relative rearward airspeed less than ___ kts.

Maximum airspeed for operation with landing gear extended

150 KCAS

Maximum speed with ramp open

260 KCAS

______ ______ prohibited with ramp open

Negative-g maneuvers

1,750 lbsin-flight

76

Maximum palletized load on ramp for ground operations movement

5,000 lbs

77

Cargo Compartment Floor limit is ___ pounds per square foot.

300

78

WARNING: Use of AUTO mode with the Utility Isolation Valve closed is prohibited. If ramp/door movement is inadvertently commanded through the cockpit ramp control rocker switch while in AUTO mode with the utility isolation valve closed, the command will not be executed until the utility isolation valve opens. This delayed action may appear to be ______ and can result in personnel injury/death and/or equipment damage if not anticipated.

uncommanded

79

Single cargo hook limited to ___ lbs.

10,000 lbs

80

Dual hook is limited to loads between ___ and ___ lbs.

2,000 and 12,500 lbs

81

Dual point maximum distribution between hooks is ___ or ___.

70/30 or 30/70

82

The external cargo hook doors are limited to: [A] ___ KCAS (latched open), [B] ___ KCAS (latched open, when being opened or closed). [A] shall not be opened or closed above ___ KCAS.

WARNING: Control inputs beyond those authorized may lead to departure of the aircraft from controlled flight that may be unrecoverable. The potential for departure at elevated angle of attack is increased with concurrent pedal inputs and/or ______ ______ application.

Flight Operations in visible moisture from 4° to -4° C

Flight Operations in visible moisture from

Fully functional IPS, or:Pitot HeatAOA HeatEAPSEngine Anti-IceFunctional Ice detectorAn official forecast of "none" or "trace" icing within ±4,000ft of the route of flight

119

Flight Operations in visible moisture from

Fully functional IPS, and:An official forecast of "none" or "trace" icing within ±4,000 ft of the route of flight.WARNING: Any ice accumulation in this temperature range shall be considered severe icing as it will exceed the capabilities of the icing system.

120

Ground Operations in visible moisture

All ice or snow on the aircraft shall be removed prior to flight. Aircraft air inlets shall be inspected for ice accumulation prior to all flights that are preceded by ground operations in icing conditions. AND:Pitot HeatAOA HeatEAPSEngine Anti-ice

121

NOTE: It is possible to get ice in the engine due to induced spray/moisture on the ground without the system detecting ice. ______ ______ will not automatically be turned on. Consideration should be given to selecting ______ ______ - ______ and just prior to takeoff return to ______.

If winds in excess of ___ kts are expected, the aircraft shall be flown away, placed in a hangar or proprotor blades and rudders removed.

90 kts

45 kts

With winds above ___ kts, the aircraft shall be placed nose into the wind to prevent possible rotor head damage.

60 kts

128

Wind Limit - Ground engine start up/shutdown

45 kts

129

Wind Limit - Any BFWS operations

45 kts

130

Wind Limit - Static FLT RDY, Fold Horizontal or Fold Vertical

60 kts

131

Wind limit - FULL STOW

90 kts

132

Without ______ ___ and the ___ ______ Receiver, the ______ shall not be used as a primary navigation source or for filing IFR.

AFC 86, -020 VOR, VOR

133

The use of type equipment code ___ prohibited.

/G

134

Flying under conditions of ______ turbulence should be avoided.

severe

135

Maximum turbulence penetration airspeed

220 KCAS

136

Turbulence penetration torque limit

At 100% Nr, ≤ 75% QmAt 84% Nr, ≤ 65% Qm

137

CAUTION: Operation of the aircraft in conditions of severe turbulence may result in ______ ______ annunciation and damage to the rotor and drive system as a result of asymmetrical gust loading. The aircraft is more susceptible to these ______ in APLN mode at high airspeeds and high torque settings in areas of severe turbulence, especially below ___ ft AGL due to orographic effects.

PRTR OVERTORQUEovertorques1000 ft AGL

138

Fuel dump is ______ ______ ______ ______.

prohibited except in emergencies

139

Fuel dump required configuration (time permitting)

WARNING: Fuel will impinge on and seep into the ramp and empennage during fuel dump operations increasing the ______ ______ ______. Aircraft commander should weigh the risk of ______ ______ ______ with fuel prior to emergency landing.

risk of firesaturating the aircraft

141

Minimum feed tank quantity

300 lbs

142

Maximum forward sponson allowable fuel split

2,500 lbs

143

During MATS refueling, the fuel level within each MATS must be monitored and ______ ______ (No auto shutoff).

manually isolated

144

Forward MATS limit

2,350 lbs

145

Mid and Aft MATS limit

2,200 lbs

146

MATS RGR Configuration (three tanks)

FWD: 2,350 lbsMID: 2,200 lbsAFT: 1,750 lbs

147

MATS RGR Configuration (two tanks)

FWD: 2,350 lbsMID: 1,900 lbs

148

MATS RGR Configuration (one tank)

FWD: 1,900 lbs

149

WARNING: Filling MATS greater than the fuel tank fill volumes will exceed the structural requirements of the tiedown restraints in the event of a crash. Exceeding these limits can cause MATS ______ ______ in a crash, resulting in personal injury or death.

restraint failure

150

WARNING: The troop seats directly ______ of the first and second MAT are not authorized for use due to loss of ______ ______ and possible head strike.